Dassault FALCON 900EX
Service difficulty reports · 73
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'FALCON900EX' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'FALCON900EX' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 2007FA0000569Transmitter · reads lowTHE AIRCRAFT WAS CLIMBING AND THE NR 3 ENGINE OIL PRESSURE INDICATION STARTED TO DROP. AT 46 PSI IT WENT RED AND THE PILOT SHUTDOWN THE ENGINE AND LANDED THE AIRCRAFT. THE OIL LEVEL WAS IN LIMITS AND NO EXTERNAL LEAKS WERE FOUND. A DIRECT READING PRESSURE SDR 2006FA0000656Engine · damagedAT FL350, AIRCRAFT EXPERIENCED A LOUD BANG AND FAILURE OF NR 1 ENGINE (ITT WENT TO RED AND N1 APPROXIMATELY 20 PERCENT). ENGINE WAS SHUTDOWN. DURING DESCENT EXPERIENCED VIBRATION IN AIR FRAME AND CONTROL COLUMN. POST FLIGHT INSPECTION REVEALED EXTENSIVE DAMSDR 2005FA0001224Cover · meltedMICROWAVE OVEN, PN 400-1338-02-L, INSTALLED, EXPERIENCED A (SMOKE EVENT) WHILE FLYING OVER TURKEY. REP EXAMINED THE UNIT ON 8/12/2005. THE MOISTURE COVER HAD OVERHEATED DURING OPERATION WITH A LIGHT LOAD. SB-MW-02, DATED 4/25/01 TO REPLACED MOISTURE COVER WSDR 2005FA0000815Probe · damagedDISCOVERED OIL LEVEL PROBE IN ENGINE OIL TANK TO HAVE ONE RIVET MISSING FROM THE DATA TAG AND THE PLASTIC END CAP CRACKED AT ONE RIVET HOLE. THE DATA TAG WAS VERY LOOSE BUT STILL ATTACHED BY THE ONE REMAINING RIVET. IF THE DATA TAG OR END CAP WERE TO COME LOSDR 2005FA0001127Light · damagedTHE AIRCRAFT WAS ON MFG SPI RAMP. THE CABIN LED LIGHT STRIP IN AFT CABIN BECAME WARM CAUSING HEAT DAMAGE TO THE LIGHT STRIP. THE LIGHT BOARD WAS SENT TO EMTEQ LIGHTING FOR EVALUATION. EMTEQ DETERMINED THE CAUSE OF THE FAILURE TO BE ELECTRO STATIC DISCHARGE SDR G1F2004F00002Tailpipe · corrodedIT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC, PAINT HAS BEEN BUBBLING AND STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON THIS SPECIFIC AC, ALL OF CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. ARESDR G1F2004F00001Tailpipe · corrodedIT HAS BEEN DISCOVERED WHILE DOING TAILPIPE INSPECTIONS ON AC. THE PAINT HAS BEEN BUBBLING AND THE STRUCTURE UNDERNEATH HAS BEEN CORRODING. ON AC, ALL OF THE CORROSION FOUND IN ALL THREE TAILPIPES HAS BEEN WHERE THE AFT ATTACH POINT MEETS THE TAILPIPE. THE SDR UO22003F00007Duct · crackedNR 2 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.SDR UO22003F00006Duct · crackedNR 3 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.(K)SDR UO22003F00005Duct · crackedNR 1 ENGINE AFT DUCT CRACKED AROUND RIB DUCTS.SDR UO22003F00010Duct · crackedNR 1 ENGINE AFT BY-PASS DUCT CRACK AROUND 9 O’CLOCK RIB DUCT, ALLOWED MOMENTARY DISENGAGEMENT OF OIL TRANSFER TUBE AND ORING FAILURE. OIL LEAK CAUSED LOSS OF OIL PRESSURE AT TAKEOFF. PILOT SHUT DOWN ENGINE AND LANDED AT NEAREST AIRPORT. AT REPLACEMENT OF SDR UO22003F00009Duct · crackedNR 2 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 OCLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAL MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)SDR UO22003F00008Duct · crackedNR 3 ENGINE AFT BY-PASS DUCT CRACKED AROUND 3 AND 9 O`CLOCK RIB DUCTS. REFERENCE TWO (2) ADDITIONAN MDR DATED 10/03/03 ON FALCON 900EX, SN032. (K)SDR 2003FA0000426Duct · damagedDURING INSPECTION NOTED PULLED RIVETS AND SPOT WELDS IN THE INTERIOR OF THE FORWARD, NR 2 ENGINE INTAKE S-DUCT ASSEMBLY. FORWARD S-DUCT ASSEMBLY WAS REPLACED WITH NEW. CAUSE OF DEFECTS IS SUSPECTED TO BE OVER PRESSURIZATION OF ANTI-ICE BLEED AIR MANIFOLD LOCSDR 811AV032403Control Panel · smokeDURING CLIMB, CREW SMELLED A BURNING ODOR AND SMOKE IN THE VICINITY OF FLIGHT GUIDANCE CONTROL PANEL. CREW TURNED OFF BACK LIGHTING TO PANEL, SMOKE AND ODOR DISIPATED. FLIGHT CONTINUED TO DESTINATION UNEVENTFUL. MAINTENANCE REMOVED AND REPLACED FLIGHT GUIDASDR 2003F00064Blocker Door · crackedDURING A ROUTINE INSPECTION OF THE THRUST REVERSER IAW THE MANUFACTURER'S OCIP PROGRAM, TWO CRACKS WERE FOUND ON THE INNER SKIN, OUTBOARD EDGE, OF THE RIGHT SIDE THRUST REVERSER BLOCKER DOOR. THE DOOR WAS REPLACED WITH A NEW DOOR PROCEDURE FROM DASSAULT AND RSDR UO22002F00015Sleeve · wornUPON INSPECTION DURING C CHECK, FOUND THAT HINGE SLEEVE WAS WORN ALMOST COMPLETELY THROUGH IF THIS PART FAILS, THE MED WILL NO LONGER BE COUNTER BALANCED AND COULD OPEN WITH GREAT FORCE AND CAUSE INJURY AND DAMAGE. CAUSE IS FROM ALL OF THE LOAD OF THE DOOR BESDR 2002FA0000812Door · stuckWHILE PERFORMING MAINTENANCE TASK 35.200, ITEM 6, SELECTION OF OXYGEN CONTROLLER TO OVERIDE, SIX PASSENGER OXYGEN MASK DOORS FAILED TO OPEN FULLY AND DEPLOY THE MASKS. FIVE OF THE DOORS OPENED APPROXIMATELY .250 INCHES AND THE SIXTH DOOR FAILED TO OPEN. INSPECSDR ROCarbon Seal · brokenTHE NR 4 CARBON SEAL CERAMIC RING WAS FOUND TO BE BROKEN DURING THE ENGINE TEARDOWN. THE CARBON RING SEAL WAS ALSO FOUND BROKEN. THERE WAS MUCH COLLATERIAL DAMAGE. THE OPERATOR REPORTED OIL LOSS DURING FLIGHT WITH SUBSEQUENT OIL CONTAMINATION UPON POST FLIGHT SDR 20010517CW007Cowling · separatedNR 1 LOWER COWLING, PN FGFB581200D2 FELL OFF IN FLIGHT 3-12-2001. LOST COWLING NOT YET RECOVERED AS OF 3-13-2001SDR 20001218SH016Pump · leakingWHILE FLYING AND INITIATING CLIMB FROM 410 TO 430, OIL PRESSURE STARTED FLUCTUATING. OIL PRESSURE CONTINUED TO FALL. ENGINE SHUT DOWN AS PRECAUTIONARY MEASURE. OIL PUMP LEAKING OIL THROUGH POROUS CASTING. (X)SDR 20000906SH002Nut · improper partUPPER RT T/R DOOR HINGE BOLT, P/N NAS6307U-23D, HAD AN ALTERNATE PART NUMBER NUT INSTALLED, P/N MS17825-7. THIS P/N NUT WAS NOT LISTED IN THE IPC (REF IPC78-30-10-10 ,ITEM 60, F12NE4753-070). ONLY THE UPPER RT T/R HINGE BOLT HAD THE ALTERNATE P/N NUT INSTALLSDR 99ZZZX4688Detector · failedLANDING GEAR FAILED TO COME DOWN ON NORMAL EXTENSION. USED EMERGENCY EXTENSION FOR GEAR DOWN, FOUND RIGHT MAIN GEAR DOOR DETECTOR FAILED 28V TEST. REMOVED AND REPLACED LEFT AND RIGHT MAIN GEAR DOOR DETECTOR. RIGHT SIDE CHANGED AS PRECAUTIONARY. PERFORMED T
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